An aircraft landing gear wheel is disclosed. A main body includes a hub portion with a gear end and an attachment end. A driven gear portion includes a first annular rail and a second annular rail, the driven gear portion being integrally and drivingly connected with the hub portion at the gear end. Rollers are rotatingly connected between roller apertures of the first annular rail and the second annular rail. Bearings rotatingly support portions of the rollers within the roller apertures.
Aircraft landing gear wheel with integral gear drive
2016-11-22
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |